ATE94950T1 - METHOD AND DEVICE FOR MAINTAINING THE EFFICIENCY OF A CATALYTIC BED IN AN ENGINE. - Google Patents
METHOD AND DEVICE FOR MAINTAINING THE EFFICIENCY OF A CATALYTIC BED IN AN ENGINE.Info
- Publication number
- ATE94950T1 ATE94950T1 AT90403013T AT90403013T ATE94950T1 AT E94950 T1 ATE94950 T1 AT E94950T1 AT 90403013 T AT90403013 T AT 90403013T AT 90403013 T AT90403013 T AT 90403013T AT E94950 T1 ATE94950 T1 AT E94950T1
- Authority
- AT
- Austria
- Prior art keywords
- catalytic bed
- engine
- maintaining
- efficiency
- impurities
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 3
- 230000003197 catalytic effect Effects 0.000 title abstract 2
- 239000000446 fuel Substances 0.000 abstract 2
- 239000012535 impurity Substances 0.000 abstract 2
- 230000006866 deterioration Effects 0.000 abstract 1
- 238000002347 injection Methods 0.000 abstract 1
- 239000007924 injection Substances 0.000 abstract 1
- 230000010355 oscillation Effects 0.000 abstract 1
- 235000011837 pasties Nutrition 0.000 abstract 1
- 239000003380 propellant Substances 0.000 abstract 1
- 239000007787 solid Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/68—Decomposition chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/56—Control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Catalysts (AREA)
- Exhaust Gas After Treatment (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Spray-Type Burners (AREA)
Abstract
Method and device for protecting a catalytic bed (4) from deterioration due to the impurities in a propellant fuel.
<??>The method consists, by briefly and periodically interrupting the supply of fuel by means of the solenoid valve (1), in creating abrupt pressure oscillations in the injection chamber (3) which expel the impurities in the pasty or possibly solid state towards the nozzle (6).
<??>Application to space vehicles.
<IMAGE>
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8914146A FR2653828B1 (en) | 1989-10-27 | 1989-10-27 | METHOD AND DEVICE FOR PROTECTING A CATALYTIC BED OF PROPELLER TRAVELED BY A FUEL FROM DEGRADATION. |
EP90403013A EP0425384B1 (en) | 1989-10-27 | 1990-10-25 | Method and device to protect the catalytic bed of a thruster from degradation |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE94950T1 true ATE94950T1 (en) | 1993-10-15 |
Family
ID=9386871
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT90403013T ATE94950T1 (en) | 1989-10-27 | 1990-10-25 | METHOD AND DEVICE FOR MAINTAINING THE EFFICIENCY OF A CATALYTIC BED IN AN ENGINE. |
Country Status (7)
Country | Link |
---|---|
US (1) | US5117627A (en) |
EP (1) | EP0425384B1 (en) |
JP (1) | JP2994450B2 (en) |
AT (1) | ATE94950T1 (en) |
DE (1) | DE69003509T2 (en) |
ES (1) | ES2045857T3 (en) |
FR (1) | FR2653828B1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5746050A (en) * | 1996-01-19 | 1998-05-05 | Primex Technologies, Inc. | Gaseous product delivery system |
US6272846B1 (en) | 1999-04-14 | 2001-08-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Reduced toxicity fuel satellite propulsion system |
US6807805B2 (en) * | 2003-03-11 | 2004-10-26 | United Technologies Corporation | Hypergolic fuel system |
US7757476B2 (en) * | 2003-07-22 | 2010-07-20 | The Aerospace Corporation | Catalytically activated transient decomposition propulsion system |
US7302792B2 (en) * | 2003-10-16 | 2007-12-04 | The Johns Hopkins University | Pulsed plasma thruster and method of making |
US20080264372A1 (en) * | 2007-03-19 | 2008-10-30 | Sisk David B | Two-stage ignition system |
US8024918B2 (en) * | 2008-04-29 | 2011-09-27 | Honeywell International Inc. | Rocket motor having a catalytic hydroxylammonium (HAN) decomposer and method for combusting the decomposed HAN-based propellant |
CN103662093B (en) * | 2013-12-20 | 2015-08-19 | 北京控制工程研究所 | A kind of orifice plate assembly for double elements thruster |
DE102014011101A1 (en) * | 2014-07-24 | 2016-01-28 | Astrium Gmbh | Injection element for a rocket combustion chamber |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3373769A (en) * | 1966-11-02 | 1968-03-19 | Moog Inc | Valve for controlling simultaneously the flow of two separate fluids |
FR2399868A1 (en) * | 1977-08-10 | 1979-03-09 | United Air Specialists | Self-cleaning electrostatic precipitator - cleaned by variable frequency vibrations produced by tank of compressed air |
US4324096A (en) * | 1979-04-23 | 1982-04-13 | Hughes Aircraft Company | Hydrazine thruster |
JPS5892729A (en) * | 1981-11-25 | 1983-06-02 | Toshiba Corp | Gas turbine combustor |
US4517798A (en) * | 1983-05-31 | 1985-05-21 | The United States Of America As Represented By The Secretary Of The Army | Porous catalytic metal plate degeneration bed in a gas generator |
US4825647A (en) * | 1983-07-26 | 1989-05-02 | Technion, Inc. | Performance improvements in thruster assembly |
US4730449A (en) * | 1983-07-26 | 1988-03-15 | Technion, Inc. | Radiation transfer thrusters for low thrust applications |
US4930310A (en) * | 1985-12-18 | 1990-06-05 | Rockcor, Inc. | Monopropellant plenum propulsion system with integrated valve/nozzle for fast response thrust |
US4766724A (en) * | 1987-06-10 | 1988-08-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Arcjet power supply and start circuit |
-
1989
- 1989-10-27 FR FR8914146A patent/FR2653828B1/en not_active Expired - Lifetime
-
1990
- 1990-10-25 ES ES90403013T patent/ES2045857T3/en not_active Expired - Lifetime
- 1990-10-25 DE DE90403013T patent/DE69003509T2/en not_active Expired - Fee Related
- 1990-10-25 AT AT90403013T patent/ATE94950T1/en not_active IP Right Cessation
- 1990-10-25 US US07/603,952 patent/US5117627A/en not_active Expired - Fee Related
- 1990-10-25 EP EP90403013A patent/EP0425384B1/en not_active Expired - Lifetime
- 1990-10-26 JP JP2290608A patent/JP2994450B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0425384A1 (en) | 1991-05-02 |
FR2653828A1 (en) | 1991-05-03 |
EP0425384B1 (en) | 1993-09-22 |
DE69003509D1 (en) | 1993-10-28 |
JP2994450B2 (en) | 1999-12-27 |
JPH03151547A (en) | 1991-06-27 |
US5117627A (en) | 1992-06-02 |
DE69003509T2 (en) | 1994-03-31 |
FR2653828B1 (en) | 1992-02-07 |
ES2045857T3 (en) | 1994-01-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |